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Title:

Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing

Document type:
Zeitschriftenaufsatz
Author(s):
Herzog, Nikolai; Keller, Dennis; Breitsamter, Christian
Abstract:
A comparison of two potential-theory based mid-fidelity approaches on the aerodynamics of a distributed propeller–wing tractor configuration is presented. The design space for aircraft configurations is enlarged by using distributed electric propulsion so a demand for investigating different variants, especially regarding the number of propellers, is present. While many lower fidelity tools are available in the literature, they are often only documented with integral results. This paper presents...     »
Dewey Decimal Classification:
620 Ingenieurwissenschaften
Journal title:
Journal of Aircraft
Year:
2024
Journal volume:
61
Journal issue:
1
Pages contribution:
196-210
Covered by:
Scopus
Language:
en
Fulltext / DOI:
doi:10.2514/1.c037313
Publisher:
American Institute of Aeronautics and Astronautics (AIAA)
E-ISSN:
0021-86691533-3868
Notes:
Acknowledgment: The authors acknowledge the financial support of the Federal Ministry for Economic Affairs and Climate Action under the framework of LuFo V-3 (FKZ:20A1706D), LuFo VI-1 (FKZ:20M1916A), and LuFo VI-2 (FKZ:20L2103A).
Submitted:
05.12.2022
Accepted:
21.08.2023
Date of publication:
01.01.2024
TUM Institution:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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